FAA AC 33.28-3 : 2014
Current
The latest, up-to-date edition.
GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS
Hardcopy , PDF
English
01-01-2014
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Chapter
1. Section 33.28 - General
2. Section 33.28(a) - Applicability
3. Section 33.28(b)(1) - Validation
4. Section 33.28(b)(2) - Environmental Limits
5. Section 33.28(c) - Control Transitions
6. Section 33.28(d) - Engine Control System Failures
7. Section 33.28(e) - System Safety Assessment
8. Section 33.28(f) - Protection Systems
9. Section 33.28(g) -Software
10. Section 33.28(h) - Aircraft-supplied Data
11. Section 33.28(i) - Aircraft-supplied Electrical Power
12. Section 33.28(j) - Air Pressure Signal
13. Section 33.28(k) - Automatic Availability and Control
of Engine Power for a 30-Second OEI Rating
14. Section 33.28(l) - Engine Shut Down Means
15. Section 33.28(m) - Programmable Logic Devices (PLD)
16. Other Considerations: Engine, Propeller and Aircraft
Systems Integration and Relations between Engine,
Propeller and Aircraft Certification Activities
Appendix 1 - References to Installation (and/or operating)
Instructions
Appendix 2 - Certification Compliance Document
Appendix 3 - Guidance for System Safety Assessment for
EECS Applied to Reciprocating Engines
Appendix 4 - Related References
Appendix 5 - Definitions
Appendix 6 - Advisory Circular Feedback Information
Specifies the general design and functioning of the ECS.
| DocumentType |
Standard
|
| Pages |
81
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
| FAA AC 00-69 : 2017 | BEST PRACTICES FOR AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
| FAA 8110.49 : 2011 | SOFTWARE APPROVAL GUIDELINES |
| FAA AC 00-66 : 2015 | SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY |
| SAE ARP5757A | Guidelines for Engine Component Tests |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
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